| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 02/25/2009 | CN101374722A Dual flow turbine engine equipped with a precooler |
| 02/24/2009 | US7493754 Gas turbine engine assembly and methods of assembling same |
| 02/24/2009 | US7493753 Gas turbine engine assembly and methods of assembling same |
| 02/18/2009 | EP2025895A2 Counter-rotatable fan gas turbine engine |
| 02/18/2009 | EP2025865A2 Fan outlet guide vane shroud insert repair |
| 02/18/2009 | CN201196120Y Hollow shaft turbojet engine |
| 02/18/2009 | CN101368511A Counter-rotatable fan gas turbine engine |
| 02/17/2009 | US7490461 Gas turbine engine assembly and methods of assembling same |
| 02/17/2009 | US7490460 Gas turbine engine assembly and methods of assembling same |
| 02/17/2009 | CA2359239C Aircraft propulsive power unit |
| 02/14/2009 | CA2632486A1 Counter-rotatable fan gas turbine engine with axial flow positive displacement worm gas generator |
| 02/11/2009 | EP2022973A1 Outer casing for a turbomachine fan conduit |
| 02/11/2009 | EP2022965A1 Axial flow fluid device |
| 02/11/2009 | EP2022949A2 Variable geometry guide vane system for the exit of a turbofan and corresponding operating method |
| 02/11/2009 | EP2022946A1 Jet engine containing a current generator mounted in the fan and an assembly method for said generator in the fan |
| 02/10/2009 | US7487630 Jet engine with compact arrangement of fan |
| 02/05/2009 | US20090035127 Valve assembly for a gas turbine engine |
| 02/04/2009 | EP2020500A2 Heat exchanger assembly for gas turbine engines |
| 02/04/2009 | EP2020499A2 Heat exchanger assembly for gas turbine engines |
| 02/04/2009 | EP2019914A1 A device for pivoting at least one pivotable element in a gas turbine engine |
| 02/03/2009 | US7484356 Cascade reverser without blocker doors |
| 02/03/2009 | US7484355 Thrust reverser comprising optimized deflector gratings |
| 02/03/2009 | US7484354 Aircraft engine arrangement |
| 01/27/2009 | US7481059 Method and apparatus for providing an afterburner fuel-feed arrangement |
| 01/26/2009 | CA2637647A1 External wall of a fan conduit in a turbine engine |
| 01/22/2009 | US20090022579 Burn resistant organic matrix composite material |
| 01/22/2009 | US20090019858 Tip turbine engine with aspirated compressor |
| 01/20/2009 | US7478525 System and method for controlling the temperature and infrared signature of an engine |
| 01/20/2009 | CA2376822C Wide angle guide vane |
| 01/15/2009 | WO2009007564A2 Turbojet engine for aircraft |
| 01/15/2009 | CA2690601A1 Turboreacteur pour aeronef |
| 01/14/2009 | EP2014901A2 Gas turbine engine with dual fans driven about a central core axis |
| 01/13/2009 | US7475546 Augmentor pilot nozzle |
| 01/13/2009 | US7475545 Fladed supersonic missile turbojet |
| 01/13/2009 | US7475532 Valve assembly for a gas turbine engine |
| 01/13/2009 | CA2409382C Blade for turbine engine |
| 01/13/2009 | CA2380779C Discharge system for simplified control turbojet or turboprop engine |
| 01/08/2009 | WO2009004143A2 Dual flow turboshaft engine and improved hot flow nozzle |
| 01/08/2009 | US20090007567 Dual Flow Turbine Engine Equipped with a Precooler |
| 01/07/2009 | EP2011988A2 Heat exchanger for a turbine engine |
| 01/07/2009 | EP2011987A2 Turbomachine with variable contour nacelle assembly and corresponding operating method |
| 01/07/2009 | EP2010773A2 Blade for a turbine |
| 01/07/2009 | EP2010757A1 Turbine blade |
| 01/06/2009 | US7472543 Jet engine noise suppressor |
| 01/01/2009 | US20090000273 Twin fan turbomachine |
| 01/01/2009 | US20090000272 Tangential anti-swirl air supply |
| 01/01/2009 | US20090000271 Gas Turbines with Multiple Gas Flow Paths |
| 01/01/2009 | US20090000270 Gas Turbines with Multiple Gas Flow Paths |
| 12/31/2008 | EP2009270A2 Gas turbine with multiple gas flow paths |
| 12/31/2008 | EP2009269A2 Gas turbine with multiple gas flow paths |
| 12/31/2008 | EP2009263A2 Tangential anti-swirl air supply |
| 12/31/2008 | EP2009262A2 Gas turbine with multiple gas flow paths |
| 12/31/2008 | EP2009261A2 Engine accessory drive system for a gasturbine |
| 12/31/2008 | EP2009260A2 Cooling system for use on aircraft |
| 12/31/2008 | CN100447397C Distribution support for service conduit in a turbofan engine |
| 12/30/2008 | US7469529 Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle |
| 12/30/2008 | US7469528 Aircraft braking method and ducted fan jet engine for implementing the method |
| 12/25/2008 | US20080315034 Turbojet Engine Nacelle with Lateral Opening of Covers |
| 12/25/2008 | US20080314047 Cooling systems for use on aircraft |
| 12/24/2008 | EP2006493A2 Aircraft combination engines thermal management system |
| 12/24/2008 | DE102008002896A1 Schubgenerator für ein Antriebssystem Thrust generator for a drive system |
| 12/24/2008 | CN100445535C Improved high-temperature turbine nozzle with light decreasement by light reflection and manufactuirng process |
| 12/23/2008 | US7467518 Externally fueled trapped vortex cavity augmentor |
| 12/17/2008 | EP2003310A2 Variable geometry nacelle for an aircraft engine |
| 12/17/2008 | EP2003309A2 Variable geometry nacelle with nanoelectromechanical system for an aircraft engine and corresponding operating method |
| 12/17/2008 | CN101326138A Metal part and brazed joint between of part produced from ceramic material |
| 12/16/2008 | US7464536 Methods and apparatus for assembling gas turbine engines |
| 12/11/2008 | US20080302083 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 12/11/2008 | DE102007026455A1 Strahltriebwerk mit Verdichterluftzirkulation und Verfahren zum Betreiben desselben Of the same jet engine with compressor air circulation and method for operating |
| 12/04/2008 | WO2008147260A1 A device for moving a plurality of hatches in a gas turbine engine |
| 12/04/2008 | WO2008105815A3 Gas turbine engine with intermediate speed booster |
| 12/03/2008 | EP1998029A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operating method |
| 12/03/2008 | EP1998028A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operation method |
| 12/03/2008 | EP1998027A2 Gas turbine engine comprising a nacelle compartment plenum for bleed air flow delivery system |
| 12/03/2008 | EP1998012A2 Access door for gas turbine engine components |
| 12/03/2008 | EP1711690B1 Gas turbine, especially an aircraft engine |
| 12/02/2008 | US7458773 Turbomachine with contrarotating fans |
| 12/02/2008 | US7458202 Lubrication system for a counter-rotating turbine engine and method of assembling same |
| 11/27/2008 | WO2008123868A3 Combined cycle missile engine system |
| 11/27/2008 | US20080290213 Turbofan Engine for Stol Aircraft |
| 11/26/2008 | EP1995468A1 Holding structure of fan blade |
| 11/26/2008 | EP1995467A1 Holding structure of fan blade |
| 11/26/2008 | EP1995443A2 Method and apparatus for regulating fluid flow through a turbine engine |
| 11/26/2008 | EP1995442A2 Turbine engine valve assembly and method of assembling the same |
| 11/26/2008 | EP1834067B1 Fan blade assembly for a tip turbine engine and method of assembly |
| 11/25/2008 | US7454894 Supplemental oil cooler airflow for gas turbine engine |
| 11/20/2008 | US20080283677 Single-stage hypersonic vehicle featuring advanced swirl combustion |
| 11/19/2008 | EP1992810A2 Variable contraction ratio nacelle assembly for a gas turbine engine |
| 11/19/2008 | EP1992807A2 Variable geometry nacelle for an aircraft engine and corresponding operating method |
| 11/18/2008 | US7451592 Counter-rotating turbine engine including a gearbox |
| 11/11/2008 | US7448845 Gas turbine engine |
| 11/11/2008 | US7448199 Self powdered missile turbojet |
| 11/11/2008 | US7448198 Gas turbine braking apparatus and method |
| 11/06/2008 | US20080271432 Sealing arrangements for gas turbine engine thrust reverser |
| 11/06/2008 | DE10145489B4 Anordnung zum Vermischen von zwei ursprünglich getrennt geführten Fluidströmen in einem Zweikreis-Strahltriebwerk Arrangement for mixing two initially separate fluid flows out in a two-circuit jet engine |
| 11/05/2008 | EP1988274A2 Turbojet engine |
| 11/05/2008 | EP1988266A2 Nacelle assembly having inlet airfoil for a gas turbine engine |
| 11/04/2008 | US7444802 Gas turbine engine including stator vanes having variable camber and stagger configurations at different circumferential positions |
| 10/30/2008 | WO2008129177A1 Method for reducing noise output at the back of a turboshaft engine and turboshaft engine improved by this method |
| 10/30/2008 | WO2008063153A3 Managing low pressure turbine maximum speed in a turbofan engine |